Novel terminal sliding mode based fault tolerant attitude control for spacecraft under actuator faults

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作者：
School of Astronautics, Harbin Institute of Technology, Harbin 150001, China [1 ]
不详 [2 ]
不详 [3 ]
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来源：
Hangkong Xuebao | / 1卷 / 249-258期
关键词：
Actuator fault - Control constraint - Control input saturation - Fault detection and isolation - Fault tolerant control - Lyapunov stability analysis - Spacecraft attitude tracking - Terminal sliding mode;
D O I：
10.7527/S1000-6893.2013.0298
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